Two-parameter bifurcation analysis of an aircraft nose landing gear model-Reference-Cited by-同舟云学术

Two-parameter bifurcation analysis of an aircraft nose landing gear model

Published:2021-01 Issue:1 Volume:103 Page:367-381
ISSN:0924-090X
Container-title:Nonlinear Dynamics
language:en
Short-container-title:Nonlinear Dyn

Author:

Cheng Lifang,Cao Hongjun,Zhang Litao

Funder

Key Scientific Research Project of Colleges and Universities in Henan Province

Aeronautical Science Foundation of China

Key Scientific Research Project of Henan Higher Education Institutions

State Key Laboratory of Traction Power

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Applied Mathematics,Mechanical Engineering,Ocean Engineering,Aerospace Engineering,Control and Systems Engineering

Link

http://link.springer.com/content/pdf/10.1007/s11071-020-06129-w.pdf

Reference19 articles.

1. Krüger, W.R., Morandini, M.: Recent developments at the numerical simulation of landing gear dynamics. CEAS Aeronaut. J. 1(1–4), 55–68 (2011)

2. Beckers, C.J.J., Öngüt, A.E., Verbeek, G., et al.: Bifurcation-based shimmy analysis of landing gears using flexible multibody models. In: Jauregui, J. (ed.) Nonlinear Structural Dynamics and Damping, pp. 261–291. Springer, Cham (2019)

3. Arreaza, C., Behdinan, K., Zu, J.W.: Linear stability analysis and dynamic response of shimmy dampers for main landing gears. J. Appl. Mech. 83(8) (2016)

4. Pacejka, H.B.: Tire and Vehicle Dynamics. Elsevier Ltd, Waltham (2012)

5. Raj, P.V.R., Santhosh, B.: Parametric study and optimization of linear and nonlinear vibration absorbers combined with piezoelectric energy harvester. Int. J. Mech. Sci. 152, 268–279 (2019)

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